Effects of 2/rev Trailing Edge Flap Input on Helicopter Vibrations for Concurrent Vibration and Noise Reduction
Alexander Steinwandel, Walter Fichter, Institute of Flightmechanics, Control
May 5, 2015
Effects of 2/rev Trailing Edge Flap Input on Helicopter Vibrations for Concurrent Vibration and Noise Reduction
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- SKU # : 71-2015-056
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Effects of 2/rev Trailing Edge Flap Input on Helicopter Vibrations for Concurrent Vibration and Noise Reduction
Authors / Details: Alexander Steinwandel and Walter Fichter, Institute of Flightmechanics and Control
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